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Free vibrations of thin-walled semicircular graphite-epoxy composite framesA detailed study is made of the effects of variations in lamination and material parameters of thin walled composite frames on their vibrational characteristics. The structures considered are semicircular thin walled frames with I and J sections. The flanges and webs of the frames are modelled by using 2-D shell and plate finite elements. A mixed formulation is used with the fundamental unknowns consisting of both the generalized displacements and stress resultants in the frames. The frequencies and modes predicted by the 2-D finite element model are compared with those obtained from experiments, as well as with the predictions of a 1-D thin walled beam finite element model. A detailed study is made of the sensitivity of the vibrational response to variations in the fiber orientation, material properties of the individual layers, and boundary conditions.
Document ID
19910004437
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Noor, Ahmed K.
(Joint Inst. for Advancement of Flight Sciences Hampton, VA., United States)
Carden, Huey D.
(NASA Langley Research Center Hampton, VA, United States)
Peters, Jeanne M.
(Joint Inst. for Advancement of Flight Sciences Hampton, VA., United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1990
Subject Category
Structural Mechanics
Report/Patent Number
L-16726
NAS 1.60:3010
NASA-TP-3010
Report Number: L-16726
Report Number: NAS 1.60:3010
Report Number: NASA-TP-3010
Accession Number
91N13750
Funding Number(s)
PROJECT: RTOP 505-63-01-11
CONTRACT_GRANT: NAG1-730
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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